|
OPERATING MANUAL
PSP 6C1A-6
SECTION 16
NAVIGATION
TABLE OF CONTENTS
Page
1. GENERAL 1
2. INERTIAL REFERENCE SYSTEM 1
3. STANDBY ARTIFICIAL HORIZON 2
4. STANDBY MAGNETIC COMPASS 2
5. WEATHER RADAR SYSTEM 2
6. RADIO ALTIMETER SYSTEM 3
7. VHF NAVIGATION SYSTEM 3
8. AUTOMATIC DIRECTION FINDER SYSTEM 3
9. DISTANCE MEASURING EQUIPMENT 4
10. AIR TRAFFIC CONTROL TRANSPONDER 4
11. FLIGHT MANAGEMENT SYSTEM 4
12. DIGITAL CLOCK SYSTEM 5
LIST OF ILLUSTRATIONS
Figure Title Page
Number
1 IRS - Simplified Block Diagram 6
2 IRS - Inertia! System Display Unit (ISDU) 7
3 IRS - Mode Select Unit (MSU) 8
4 IRS - Annunciators and Switch/Lights 9
5 IRS - Normal EFIS Displays 10
6 IRS - Failure EFIS Displays 11
7 IRS - Reversionary EFIS Displays 12
16 - CONTENTS
Page 1
Apr 10/95
cftauencjer
OPERATING MANUAL
PSP 601A-6
Figure
Number Title Page
8 Standby Artificial Horizon 13
9 Standby Magnetic Compass 14
10 Weather Radar System - Simplified Block Diagram 15
11 Weather Radar System Controller 16
12 Weather Radar System Selection/Control - EFIS MFD Controller 17
13 Weather Radar System Selection/Control - EFIS Display Controller 18
14 Weather Radar System - MFD Displays (2 Sheets) 19
15 Weather Radar System - Test Pattern 21
16 Weather Radar System - EHSI Displays 22
17 Radio Altimeter System - Simplified Block. Diagram 23
18 Radio Altimeter System - EFIS Displays 24
19 Radio Altimeter System Control - EFIS Display Controller 25
20 VHF/NAV System - Simplified Block. Diagram 26
21 VHF/NAV System Control and Remote Switch/Lights 27
22 VHF/NAV System Source Selection - EFIS Display Controller 28
23 VHF/NAV System - EADI Displays 29
24 VHF/NAV System - EHSI Full Compass Display 30
25 VHF/NAV System - EHSI MAP Display 31
26 VHF/NAV System - EFIS Failure Displays 32
27 VHF/NAV System Audio Selection/Control - Audio Integrating System 33
28 ADF System - Simplified Block Diagram 34
29 ADF System Control Unit 35
30 ADF System Source Selection - EFIS Display Controller 36
31 ADF System EFIS Displays 37
32 ADF System Audio Selection/Control - Audio Integrating System 38
16-CONTENTS
Page 2
Apr 02/87
canaaair
cnaiiertQer
OPERATING MANUAL
PSP 601A-6
Fi gure
Number Title Page
33 DME System - Simplified Block Diagram 39
34 DME System Selection/Control - VHF/NAV Control 40
35 DME System - EFIS Displays 41
36 DME System Audio Selection/Control - Audio Integrating System 42
37 ATC Transponder System Control Unit 43
38 FMS - Simplified Block Diagram 44
39 FMS Control Display Unit (CDU) (2 Sheets) 45
40 FMS EHSI Source Selection - EFIS Display Controller 47
41 FMS - Remote Annunciators 48
42 FMS - EADI Display 45
43 FMS - EHSI Full Compass Display (2 Sheets) 50
44 FMS - EHSI MAP Display (Additional Displays) 52
45 FMS MFD Source Selection and Display Control - EFIS MFD Controller 53
46 FMS - MFD MAP Display 54
47 FMS - MFD PUN Display 55
48 Digital Clock Controls 56
16-CONTENTS
Page 3
Apr 02/87
OPERATING MANUAL
PSP 601A-6
SECTION 16
NAVIGATION
1. GENERAL
The following systems and components are used for navigation:
Inertia! reference system (IRS)
Standby magnetic compass
Standby horizon indicator
Weather radar system
Radio altimeter system
VHF navigation (VHF/NAV) system
Automatic direction finder (ADF) system
Distance measuring equipment (DME) system
Air traffic control (ATC) system
Flight management system (FMS)
Digital clock
2. INERTIAL REFERENCE SYSTEM (Figures 1 through 7)
The laser inertia! reference system (LIRS) is a dual system (IRS 1 and IRS 2)
which provides aircraft present position, attitude, velocity, heading data,
wind speed, wind direction and ground speed data. The LIRS interfaces with
the flight management systems (FMS 1 and FMS 2), the electronic flight
instrument system (EFIS), the weather radar system, the automatic flight
control system (AFCS) and the digital air data system (DADS).
Initialization data {latitude and longitude) is entered into the LIRS from
| either the inertia! system display unit (ISDU) or the FMS (refer to
paragraph 11.).
IRS REV switch/lights are located on the pilot's and copilot's instrument
panels, to provide for selection of the on-side or cross-side IRS.
The system includes two inertia! reference units (IRU), a six-annunciator
mode select unit (MSU) for each IRU, an inertia! system display unit (ISDU),
and a blower kit and backup battery for each IRU- It also has full
| provisions for a third inertia! reference unit (IRU 3).
SECTION 16
Page 1
Apr 10/95
ctianencter
OPERATING WUfJAL
PSP 601A-6
STANDBY ARTIFICIAL HORIZON (Figure 8)
The artificial horizon indicator displays pitch and roll aircraft attitude
information- Vertical attitude is maintained by a mechanical erection system.
The indicator continues to provide attitude information for a minimum of 9
minutes after loss of power.
STANDBY MAGNETIC COMPASS (Figure 9)
The standby magnetic compass is aligned with the
is of the self-contained, dry type. A miniature
heading against a rotating vertical compass card.
aircraft longitudinal axis and
aircraft pointer displays the
WEATHER RADAR SYSTEM (Figures 10 through 16)
The weather radar system detects and locates various types of weather along the
flight path of the aircraft and provides a visual indication of the storm
intensity on the multifunction display (MFD). Weather radar functions are
controlled by the weather radar controller. The EFIS MFD controller provides
for selection and dimming control of the weather radar display on the MFD. The
weather radar returns can also be displayed on the pilot's and copilot's
electronic horizontal situation indicators (EHSI) in the partial compass mode,
selectable from the pilot's and copilot's display controllers. The weather
radar system also has a supplementary ground mapping function to assist with
navigation and should not be used or relied upon for proximity warning,
anti-collision or tension avoidance. The colours used in the weather and
ground mapping modes are as follows.
HEATHER
Level 0
Level 1
Level 2
Level 3
Level 4
Level 0
Level 1
Level 2
Black
Green
Yellow
Red
Magenta
GROUND MAPPING
Black
Cyan
Yellow
No reflective target
Least rainfall
Heavy rainfall
Next heaviest rainfall
Heaviest rainfall
No reflective target
Least reflective target
Next level of reflective
target
Level 3 Magenta Most reflective target
SECTION 16
Page 2
Apr 02/87
cacnhaadJaleirn Qer
OPERATING MANUAL
PSP 601A-6
The attitude source used by the weather radar system is controlled by the IRS
REV pushbutton on the pilot's instrument panel. The weather radar system is
inhibited when the aircraft is on the ground. The weather radar system
consists of the receiver/transmitter/antenna and the weather radar
controller.
RADIO ALTIMETER SYSTEM (Figures 17, 18 and 19)
The radio altimeter system is a high-resolution, short-pulse radio altitude
system that provides precise information on ground proximity during the
approach and landing phases of aircraft operation. Radio altitude is
displayed on the pilot's and copilot's electronic attitude director
indicators (EADIs).
The radio altimeter system consists of a transmitter/receiver, transmitter
antenna and receiver antenna.
On aircraft 5041 and 5146,
the radio altimeter system is dual and consists of two transmitter/receivers,
two transmitter antennas and two receiver antennas.
VHF NAVIGATION SYSTEM (Figures 20 through 27)
The VHF navigation (VHF/NAV) systems No. 1 and No. 2, receive and process VHF
omnirange (VOR), localizer (LOC), glideslope (GS) and marker beacon signals
to provide short-range navigation (SRN) for the pilot's and copilot's
systems. The VHF/NAV systems No. 1 and No. 2, provide VOR, LOC and GS
deviation, V0R/L0C audio, VOR bearing, VOR TO/FROM data and marker beacon
outputs. The VHF navigation information is used by the electronic flight
instrument system (EFIS), the flight management system (FMS), automatic
flight control system (AFCS) and the audio integrating system.
The pilot's and copilot's display controllers provide for selection of the
VHF/NAV system information.
AUTOMATIC DIRECTION FINDER SYSTEM (Figures 28 through 32)
The automatic direction finder (ADF) systems No. 1 and No. 2 receive signals
from the selected ground station, to provide relative bearing to the station
for display on the pilot's and copilot's electronic horizontal situation
indicators (EHSI) and audio signals for the intercom system. The station
selected can be a non-directional beacon or a standard AM broadcast station
operating in a frequency range of 190 to 1799.5 kHz.
The pilot's and copilot's source controllers provide for selection of the ADF
information displayed on EFIS. The ADF system consists of two ADF receivers,
two ADF control units and a dual ADF antenna.
SECTION 16
Page 3
Aug 14/02
cacnhaadTaleirn qer
OPERATING MANUAL
PSP 601A-6
9. DISTANCE MEASURING EQUIPMENT (Figures 33 through 36)
The distance measuring equipment (DME 1 and DME 2) measures the slant range
distance between the aircraft and the tuned DME ground station, up to 300
nautical miles. The distance information is supplied to the electronic flight
instrument system (EFIS) and the automatic flight control system (AFCS). The
DME 1 and DME 2 also provide ground speed, time-to-station and ground station
identification data outputs for the flight management system No. 1 (FMS 1) and
the flight management system No. 2 (FMS 2 ) , respectively, and audio outputs
for the intercom system.
The DME 1 and DME 2 can be tuned manually or automatically. Manual tuning is
performed from the VHF/NAV control in short-range radio navigation. Automatic
tuning is performed by the FMS in long-range FMS navigation. The pilot's and
copilot's EFIS source controllers provide for selection of the DME distance
displayed on EFIS and used by the flight director system (FDS) and the air data
system (ADS) when the short-range radio navigation is used. The DME distance is
switched in conjunction with the VHF/NAV system data (refer to paragraph 7.).
The DME consists of the two transmitter/receivers and two antennas. Control
of the DME 1 and DME 2 is provided by the VHF/NAV systems No. 1 and No. 2.
10. AIR TRAFFIC CONTROL TRANSPONDER (Figure 37)
The air traffic control (ATC) transponder system provides the ATC ground radar
systems with coded identification and altitude data in response to a valid
interrogation signal. This enables the air traffic controller to identify
transponder-equipped aircraft in addition to detecting range and direction.
The ATC transponder system uses altitude data from the air data system No. 1
(ADS 1) and from the air data system No. 2 (ADS 2 ) . The ATC transponder
control unit provides for control of the ATC transponder systems.
The ATC transponder system consists of two transponders, a control unit, a
control adapter and two antennas.
11. FLIGHT MANAGEMENT SYSTEM (Figures 38 through 47)
The flight management systems No. 1 and No. 2 (FMS 1 and FMS 2) use navigation
data including attitude and heading from the inertial reference system (IRS),
altitude, true airspeed (TAS) and static-air-temperature (SAT) from the air
data system (ADS), and distance information from the scanning distance
measuring equipment (DME) system, in order to navigate the aircraft along a
programmed flight plan. The programmed flight plan is computed by the flight
management system (FMS) navigation computer unit (NCU) and displayed and
controlled by the FMS control display unit (CDU). The FMS interfaces with the
electronic flight instrument system (EFIS) and the flight guidance system (FGS)
to display and control the FMS computed flight plan. The FMS 1 and FMS 2 also
use fuel flow inputs from the fuel flow sensors to provide for fuel management.
SECTION 16
Page 4
Apr 02/87
OPERATING MANUAL
PSP 601A-6
The p i l o t s and copilot's EFIS source controllers provide for selection of the
FMS navigation data and FMS bearing displayed on EFIS, and the roll steering
command applied on the on-side flight director system (FDS). The multifunction
display (MFD) provides for selection of the FMS navigation data displayed on
the MFD.
The FMS 1 and FMS 2 provide tune control serial data to the associated VHF
navigation (VHF/NAV) system to automatically tune the DME receiver in order to
provide the scanning DME function.
12. DIGITAL CLOCK SYSTEM (Figure 48)
Both the pilot and copilot have a digital clock system. The clocks can be set
to display local, flight and elapsed time. Each clock is powered by a 6-volt
battery.
The digital clock systems consist of a digital clock, a press-to-reset switch
and a resistor.
SECTION 16
Page 5
Apr 02/87
OPERATING MANUAL
PSP 601A-6
FMS1
TO EADI, EHSl,
EFIS. AFCS AND FMS
ISDU
PILOTS
SIDE
CONSOLE
FMS 2
tl
URU
NO. 1
PILOTS
INSTRUMENT
PANEL
REV
T
IRS
1
COPILOTS
SIDE
CONSOLE
I
WEATHER!
RADAR
* ^ r ffiS
2
COPILOTS
SIDE
CONSOLE
LIRU
NO. 2
ASCB BUS
mm __t wotx*s^^^ I I
COPILOTS
INSTRUMENT
PANEL
COPILOTS
MSU
m* ^ o PILOTS
EADI
^
m
* M *
X
PILOTS
EHSi
MFD
COPILOTS
EAD!
COPILOTS
EHSl
DADC
NO. 2
IRS - Simplified Block Diagram
Figure 1
SECTION 16
Page 6
Apr 02/87
chauenper
OPERATING MANUAL
PSP 601A-6
Honeywell LASEREF
ZL i_ i i
^
DIMMER KNOB
Controls the brightness of
the display.
DSPL SEL SWITCH
Selects the data to be shown on the
digit display.
TEST - lights all the display
elements and the keyboard ENT and
CLR cue tights. The switch is springloaded
and must be held in this
position.
TK/GS - Selects the track angle in
degrees on the left display and the
ground speed in knots on the right.
PPOS - Selects the latitude on the
left display and the longitude on the
right.
WIND - Selects the wind direction
in degrees on the left display and the
wind speed in knots on the right.
HDG/STS - Selects true or
magnetic heading on the left display
and time to complete alignment on
the right.
DSPLSEL
*> OS WIND
TK/GsVv^—-^ .HDG/STS
E^
SYS DSPL SWITCH
Selects the IRU from which
the displayed data originates.
If the switch is set of OFF.
the ISDU cannot send or
receive data to or from any
IRU.
H
Q•
p
•CO •H
S3 m
El
iy]
DIGIT DISPLAY
Shows data from the
selected system.
KEYBOARD
Enters initial data.
ENT AND CLR KEYS
Contain green cue lights
which, when lit. indicate that
operator action is required.
CLR is used to remove data
erroneously entered. ENT is
used to send data to the
IRU.
PILOTS SIDE CONSOLE
IRS - Inertial System Display Unit (ISDU)
Figure 2
SECTION 16
Page 7
Apr 02/87
OPERATING MANUAL
PSP 601A-6
NAV RDY ANNUNCIATOR
Comes on to indicate that
the alignment is complete.
ALIGN ANNUNCIATOR
Light iUurninates when the
mode select switch b in the
ALIGN position (mode). The
light -flashes, if alignment
requirements are not met
because of aircraft movement
or incorrect operator action.
FAULT ANNUNCIATOR
Comes on to indicate that
there is a fault in the IRS.
NO AIR ANNUNCIATOR
Comes on to indicate a
cooling loiiure.
TEST PUSHBUTTON
initiates a test sequence m
which the IRS outputs three
sets of specified test va»u»
sequentially. Used for
maintenance purposes
MODE SELECT SWITCH
Selects the four IRU basic modes
and the four submodes. NAV
position is detented.
OFF - Turns off the IRS
ALIGN - Turns the IRS on and
selects the align mode. To complete
the align mode, inputs the initial
position latitude and longitude must
entered into the IRS, either from the
FMS or from the ISDU.
NAV - Seleos the navigation mode
if the align mode is successfully
completed.
ATT - Selects the revisiohary ATT
(attitude) mode for the IRS. normally
used when the NAV mode fails.
ON BATT ANNUNCIATOR
Comes on to indicate that
the IRS is receiving power
from the IRS back-up
battery.
BATT CAIl Ahi.\:jN?:A'r;,..
Comes on to indicate that
the IRS back-up battery is
supplying less than the
minimum voltage required for
IRS operation.
CENTRE PEDESTAL
IRS - Mode Select Unit (MSU)
Figure 3
SECTION 16
Page 8
Apr 02/87
OPERATING MANUAL
PSP 601A-6
IRS
REV
IRS REV SWTTCH/UGHT
When preeaod, eeiects the cross-tide
IRS as back-up when the on-side
IRS source fails.
PILOTS AND COPILOTS INSTRUMENT PANELS
b Att/lLIAfpY BATTERY
IRS
1
IRS
2
IRS
3
CHARGER FAIL
BATT/CHARGER FAIL
ANNUNCIATOR
Comas on (ember) to indicate that
the back-up battery is not charging.
d
EFFBCnVTTY: A/C 5136 AND SUBS AND A/C POST SB 601 - 0 * 16
2
BATT/CHARGER FAIL
ANNUNCIATOR
Comas on iember) to indicate that
the back-up battery b not charging.
/
FAIL I
ON I
\U XILlAr/y BATTERY
I IRS I
1
I IRS I
2
I IRS I
BlNOPl
APU BATT/CHARGER FAIL
EFFECTMIY: A/C 8001 TO SIS*
d
COPILOTS CONSOLE
IRS - Annunciators and Switch/Lights
Figure 4
SECTION 16
Page 9
Apr 10/95
OPERATING MANUAL
PSP 601A-6
WIND VECTOR DISPLAY
Indicates wind speed and direction
calculated by the IRS.
HEADING SOURCE ANNUNCIATOR
A white MAG annunciation is
displayed above the heading dial to
indicate that the heading source is
referenced to magnetic North.
HEADING DIAL
Displays magnetic IRS heading.
EHS!
GSPD DISPLAY
Indicates ground speed calculated by
the IRS (see note).
ATTITUDE SPHBIE
Displays IRS pitch and roll attitude.
NOTE
Ground speed is supplied by the
PMS when en FMS navigation
source is selected.
HAD!
PILOTS AND COPILOT'S INSTRUMENT PANELS
IRS - Normal EFIS Displays
Figure 5
SECTION 16
Page 10
Apr 02/87
ctvanenaer
OPERATING MANUAL
PSP 601A-6
Y f
o IRS
V
160
DH200
I I
s: LA
J
//
/y
IRS ATTITUDE FAILURE
When the IRS fails, the pitch scale
and roil pointer are removed, the
flight director command bars are
removed, the attitude sphere is
removed and a red boxed IRS
annunciation is displayed in the
centre of the EAD1.
/ . V
jo
!
i
\
f m 1
CRS L1r^ HDG
349 ^xMM'/v- 340
0 c j:
R - ^ -j- "i—-
1 r + -£
180 ' ' W . l . ^ ]TG
RNE 1 34-5 >n m
* o
^
IRS HEADING FAILURE
When the IRS fails, the MAG
annunciation, heading bug. course
select/desired track pointer, scale
and deviation bar. to-from pointer.
bearing pointers are removed. The
heading dial is displayed North up
and a re6 boxed IRS is displayed
above the heading dial.
PILOT'S AND COPILOTS INSTRUMENT PANELS
IRS - Failure EFIS Displays
Figure 6
SECTION 16
Page 11
Apr 02/87
OPERATING MANUAL
PSP 601A-6
IRS REVERSION ANNUNCIATOR
When the cross-side IRS is
transferred to the on-side, an amber
boxed XIRS is displayed on the on
side EHSl and EAOi and an amber
boxed green IRS is displayed on the
cross-side EHSl and EADL
PILOTS AND COPILOTS INSTRUMENT PANELS
IRS - Reversionary EFIS Displays
Figure 7
SECTION 16
Page 12
Apr 02/87
ctiafiencjer
OPERATING MANUAL
PSP 601A-6
ROLL INDEX
POWER WARNING FLAG
Comes into view to indicate a caged
condition, standby artificial horizon
failure or a power loss.
ROLL POINTER
HORIZON LINE
DRUM
PITCH - TRIM SCALE
AIRCRAFT
SYMBOL
CAGING/PITCH - TRIM KNOB
When pulled, the indicator is caged.
When rotated, the aircraft symbol is
adjusted for varying pitch attitudes.
CENTRE INSTRUMENT PANEL
Standby A r t i f i c i a l Horizon SECTION 16
Figure 8 Page 13
Apr 02/87
canadair
ctianencjer
OPERATING MANUAL
PSP 601A-6
BELOW OVERHEAD PANEL
Standby Magnetic Compass SECTION 16
Figure 9 page 14
Apr 02/87
cftauencjer
OPERATING MANUAL
PSP 601A-6
AIR/GND
MODULE
WOW
WEATHER
RADAR
SYSTEM
ATTITUDE
PILOT'S
DISPLAY
CONTROLLER
WX DISPLAY VIDEO
EF1S MFD
CONTROLLER
WX DISPLAY VIDEO
COPILOTS
DISPLAY
CONTROLLER
WX DISPLAY VIDEO
PILOTS
INSTRUMENT
PANEL
URS1
J **
*f **
URS2
--J psl
jREVli
PILOTS EHSI
°s&o
O
z WX DIM CONTROL
MFD
f \ ..-5-,
•
V
, fi *L_
^"\
. /
OVERALL DIM CONTROL
COPILOTS EHSI
WX DIM CONTROL
Weather Radar System - Simplified Block Diagram
Figure 10
SECTION 16
Page 15
Apr 02/87
OPERATING MANUAL
PSP 601A-6
RANGE PUSHBUTTONS
The two range pushbuttons allow
range selection from 5 to 300 NM
full scale in the ON mode, or from 5
to ?000 NM fullscale in the FP mode.
The up arrow pushbutton selects
increasing ranges, and the down
arrow pushbutton selects decreasing
ranges.
RCT PUSHBUTTON
Selects rain echo attenuation
compensation techntQue (RCT
mode). When the RCT mode is
disabled, the OFF annunciator above
the pushbutton comes on.
STAB PUSHBUTTON
Allows the antenna stabilization
inputs to be disabled. When the
inputs are disabled, the stabilization
off condition is indicated by the OFF
annunciator above the switch.
TGT PUSHBUTTON
Enables/disables target alert mode.
SECT PUSHBUTTON
Selects eitner tun azimuth scsr. i uu
degrees) or sector azimuth scan (60
degrees).
GAIN/PRESET CONTROL
Adjusts radar receiver gain.
MODE SELECTOR
Selects weather radar operating
modes.
WX/MAP SELECTOR
Selects weather or map display
when the mode selector is in the ON
position.
TILT CONTROL
Adjusts antenna tilt angle.
CENTRE PEDESTAL
Weather Radar System Controller SECTION 16
Figure 11 Page 16
Apr 02/87
canadair
ctiaiiencjer
OPERATING MANUAL
PSP 601A-6
WX PUSHBUTTON
Selects weather radar
information for display on
MFD indicator.
MODE (OUTER) SELECTOR
Controls MFD indicator display
brightness.
CENTRE PEDESTAL
Heather Radar System Selection/Control -
EFIS MFD Controller
Figure 12
SECTION 16
Page 17
Apr 02/87
OPERATING MANUAL
PSP 601A-6
WX PUSHBUTTON
Selects weather radar returns for display on the
SHS1. If the full compass is displayed prior to WX
selection, pressing the WX pushbutton automatically
selects the partial compass for display with the
weather redar returns.
WX DIM (INNER) CONTROL
Adjusts the brightness of the
weather radar r e t i r e v . :he EHSi.
PILOTS AND COPILOTS SIDE PANELS
Heather Radar System Selection/Control -
EFIS Display Controller
Figure 13
SECTION 16
Page 18
Apr 02/87
ctiauenaer
OPERATING MANUAL
PSP 601A-6
WEATHER RADAR DISPLAY
AZIMUTH
LINE
RANGE
WEATHER
DISPLAY
RANGE
RING
WEATHER
RADAR
MODE
AIRCRAFT
SYMBOL
CENTRE INSTRUMENT PANEL
Weather Radar System - MFD Displays
Figure 14 (Sheet 1)
SECTION 16
Page 19
Apr 02/87
OPERATING MANUAL
PSP 601A-6
COMPASS ARC
(WHITE)
MAG/TRU
(WHITE)
VOR SELECTION
ANNUNCIATOR
(MAGENTA)
APT SELECTION
ANNUNCIATOR
(MAGENTA).
RANGE
(CYAN)
(GREEN)
SELECTED
NAV SOURCE
(GREEN)
WX RETURN
DISPLAY
WX MODES
(CYAN)
WAYPOIN1
'PENTS
(WHITE)
NAV DATA
(MAGENTA)
TO WAYPOINT
DATA
(GREEN)
DESIGNATOR
(WHITE)
(CYAN IF OFFSET)
CROSSTRACK
DEVIATION
(GREEN)
MAP WITH WEATHER RADAR DISPLAY
CENTRE INSTRUMENT PANEL
Heather Radar System - MFD Displays
Figure 14 (Sheet 2;
SECTION 16
Page 20
Apr 02/87
canaaair
ctiauenoer
OPERATING MANUAL
PSP 601A-6
WXMODE
ANNUNCIATORS
• STBY (GREEN)
• TEST (GREEN)
• WX (GREEN)
• RCT (GREEN)
• GMAP (GREEN)
» FAIL (AMBER)
TGT OR VAR ANNUNCIATOR
• TGT: TARGET ALERT
- GREEN-SELECTED
- AMBER-LVL3 OR 4 TGT DETECTED]
• VAR: VARIABLE GAIN (AMBER)
WX RANGE TGT ALT ON: RED
RINGS TGT ALT OFF: BLACK
(WHITE) AND NOISE BAND
ANTENNA
TILT
ANGLE
REACT OFF: BLACK
REACT ON: BLUE
REACT
FIELD
WX RANGE
ANNUNCIATOR
(WHITE)
REACT OFF: NOISE
REACT ON: MAGENTA
NOISE
REACT OFF: BLACK
REACT ON: BLUE
MAGENTA
RED GREEN YELLOW
CENTRE INSTRUMENT PANEL
Weather Radar System - Test Pattern
Figure 15
SECTION 16
Page 21
Apr 02/87
OPERATING MANUAL
PSP 601A-6
TARGET ALERT
ANNUNCIATOR
RANGE
RING
MODE
ANNUNCIATOR
WX RETURN
DISPLAY
RANGE
ANNUNCIATOR
PILOTS AND COPILOTS INSTRUMENT PANELS
Weather Radar System - EHSI Displays
Figure 16
SECTION 16
Page 22
Apr 02/87
canaaair
cfiauencier
OPERATING MANUAL
PSP 601A-6
RADIO
ALTIMETER
SYSTEM
TEST GROUND
m " % r ™ - •
RADIO ALTITUDE
PILOT'S EFIS
DISPLAY
• —45
< Hl»
6
TEST
COPILOT'S EFIS
DISPLAY
CONTROLLER
-A
< -Hl»
6
1 TEST
-f
J
V
w~ -•
PILOT'S EAD1
J ± t t ^
COPILOTS EADI
Radio Altimeter System - Simplified Block Diagram
Figure 17
SECTION 16
Page 23
Apr 02/87
OPERATING MANUAL
PSP 601A-6
O*. CATION
Displayed in amber when the aircraft
is at or below the selected decision
height.
2vC" a.<;i the Display c bumUeo. When •— .-*•<
altimeter fads a red boxed RA annunciator ;s
displayed and the radio altitude information is
removed. When m the test mode, the radio a>~
cSsolay indicates a test value of 100 feet
LOCALIZER POINTER/RISING RUNWAY
indicates localizer deviation when the selected
navigation source is tuned to a localizer frequency.
At 200 feet or less, the pointer becomes the rising
runway. When the on-side navigation source is
selected the pointer/rtsmg runway is green. When
the cross-side source is selected, the pointer/rismg
runway is yeHow.
DH DISPLAY
Indicates the selected decision
height from 0 to 990 feet in 10 foot
increments.
PILOTS AND COPILOTS INSTRUMENT PANELS
Radio Altimeter System - EFIS Displays
Figure 18
SECTION 16
Page 24
Apr 02/87
cacntaiaanaeirn per
OPERATING MANUAL
PSP 601A-6
DH/TST CONTROL/SWITCH
Rotation of the DH/TST control/switch allows the decision
height display on the EADt to be adjusted. Rotating the
control fully counterclockwise removes the decision height
display from the EADi.
Pressing the DH/TST control/switch initiates the test mode.
On the ground. EF1S and the radio altimeter are checked. In
flight, only the radio altimeter is checked, provided the GS
mode is not captured.
PILOTS AND COPILOTS SIDE PANELS
Radio Altimeter System Control - SECTION 16
EFIS Display Controller Page 25
Figure 19 Apr 02/87
OPERATING MANUAL
PSP 601A-6
VHF/NAV System - Simplified Block Diagram
Figure 20
SECTION 16
Page 26
Apr 02/87
cacnhaaciietaniQr er
OPERATING MANUAL
PSP 601A-6
MKR/BCN
HIGH
LOW
MKR/BCN HIGH/LOW
SWITCH/LIGHT
Select the receive sensitivity
for the marker beacon receiver
PILOTS AND COPILOTS INSTRUMENT PANELS
ACT ANNUNCIATOR
Comes on while the active frequency
is changed. Stays on flashing if the
tuning is incorrect.
PRESET FREQUENCY DISPLAY
Displays preset (inactive} frequency
and diagnostic messages. Shows
DME frequency when HLO is
selected.
MEMORY ANNUNCIATOR
Comes on when a preset frequency
is shown in the preset frequency
display.
RMT ANNUNCIATOR
Comes on while the DME is remotely
tuned by the FMS.
/ /_/ /_/ /_/ /_/
i. o O O O
I U U. U U
MEM ^ RMT
XFR,
ACT PUSHBUTTON
POWER AND MODE SELECTOR
OFF - Removes power from the
DME and VOR systems.
ON - Applies power to the DME and
VOR systems.
HID - Holds the DME on the
selected frequency white the
VHF/NAV frequency is changed.
ACTIVE FREQUENCY DISPLAY
Displays active frequency and
diagnostic messages.
XFR/MEM SWITCH
Allows transfer of a preset frequency
into the active display (XFR
position). Loads stacked memory
frequency into preset display (MEM
position).
HLD ANNUNCIATOR
Comes on to indicate that the DME
is held whHe VHF/NAV frequency is
changed.
FREQUENCY SELECTORS
Selects the DME and VOR
frequencies simultaneously.
Enables the frequency selectors to
directly tune the DME and
VHF/NAV.
LIGHT SENSOR
Automatic display
STORE PUSHBUTTON
Allows preset frequencies to be
selected and entered into memory.
CENTRE PEDESTAL
VHF/NAV System Control and Remote Switch/Lights SECTION 16
Figure 21 Page 27
Apr 02/87
OPERATING MANUAL
PSP 601A-6
V/L PUSHBUTTON
Selects between the VHF/NAV
system No. 1 and VHF/NAV system
No. 2 as the short range navigation
(SRN) source.
BR6 0 SELECTOR
When set to VOR 1, the associated
bearing pointer on the EHSI displays
the bearing to the station tuned on
the VHF/NAV system No. 1.
BRG O SELECTOR
When set to VOR 2. the associated
bearing pointer on the EHSi displays
the bearing to the station tuned on
the VHF/NAV system No. 2.
PILOTS A N D COPILOT'S SIDE PANELS
VHF/NAV System Source Selection -
EFIS Display Controller
Figure 22
SECTION 16
Page 28
Apr 02/87
ctiaH&ncjer
OPERATING MANUAL
PSP 601A-6
MARKER BEACON ANNUNCIATIONS
Indicates marker beacons as follows:
Outer marker beacon = 0M (cyan)
Middle marker beacon = MM (yellow)
inner marker beacon = IM (white)
LOCALIZER POINTER/RISING RUNWAY
Indicates localizer deviation when the
selected VHF/NAV source is tuned to a
localizer frequency. At 200 feet or less.
the pointer becomes the rising runway.
The localizer pointer is displayed in green
or yellow (consistent with the distance
display).
GUOESLOPE POINTER AND SCALE
Displays glideslope deviation. The scale is
displayed in white and the pointer is
displayed in green or yellow (consistent
with the distance display}.
PILOTS AND COPILOTS INSTRUMENT PANELS
VHF/NAV System - EADI Displays
Figure 23
SECTION 16
Page 29
Apr 02/87
OPERATING MANUAL
PSP 601A-6
COURSE PRESELECT SOURCi
ANNUNCIATOR
Indicates the source of the course
prasetect information. Displayed in
magenta.
NAVIGATION SOURCE ANNUNCIATOR
Indicates the navigation source selected.
Displayed in green or yellow (consistent
with the distance display}.
BEARING SOURCE
ANNUNCIATORS
Indicates the selected bearing
source for the associated
bearing pointer.
A = ADF
F = FMS
V = VOR
The colour of the bearing
source annunciators
co jspond to the bearing
pointers.
DISTANCE DISPLAY
Displays the DME distance to the selected
VHF/NAV source. When the on-side
VHF/NAV source is selected, the
Usance display is green. When the
cross-side VHF/NAV source is selected.
the display is yellow.
BEARING POINTER NO. 1
Indicates the bearing to the
source selected by the BRG O
control.
BEARING POINTER NO. 2
Indicates the bearing to the
selected by the BRG^
Displayed in white.
TO/FROM ANNUNCIATOR
Indicates whether the aircraft is
moving towards or away from
the VOR station. Displayed in
green or yellow (consistent with
the distance display).
GUDESLOPE POINTER AND
SCALE
SeeEADI.
COURSE DEVIATION BAR AND POINTER
Indicates aircraft deviation from the vOfi
or localizer beam. The pointer is displayed
in green or yellow (consistent with the
distance display).
COURSE PRESELECT
DEVIATION BAR AND
POINTS?
Indicates aircraft deviation f w i
thepie.ieiewt--f'k-.ai.'-» •—• --
setecrc'j.
PILOTS AND COPILOTS INSTRUMENT PANELS
VHF/NAV System - EHSI Full
Figure 24
Compass Display SECTION 16
Page 30
Apr 02/87
canadaar
czhauencier
OPERATING MANUAL
PSP 601A-6
SELECTED COURSE LINE
indicates the selected course to the
VOR/DME station. The solid line
segment indicates the TO side and
the broken line segment indicates
the FROM side. When the station is
outside the display range, an
arrowhead is added to the end of
the course line. The course line is
displayed in green when the selected
VHF/NAV source is on-side and in
yellow when the selected VHF/NAV
source is cross-side.
VOR/DME NAVAIDS
Indicate the location of the
VOR/DME stations. When the
VOR/DME station corresponds u.
the selected navigation source, a
number (1 or 2) is displayed next to
the navaid symbol. The navaid
symbol corresponding to the BRG O
selector setting, is displayed in
cyan. The navaid symbol
corresponding to the BRG O
selector setting, is displayed in
white.
CROSS-TRACK DEVIATION
DISPLAY
Indicates the aircraft deviation from
the selected course in nautical miles.
Displayed in green or yellow
(consistent with the selected course
line).
PILOT'S AND COPILOT'S INSTRUMENT PANELS
NOTE
The MAP mode provides the same information as the full compass
mode, except that the course pointer, scale and deviation bar are
removed and a partial compass is displayed with the additional
information indicated in this figure.
VHF/NAV System - EHSI MAP Display
Figure 25
SECTION 16
Page 31
Apr 02/87
OPERATING MANUAL
PSP 6U1A-6
NAvioAHON SOURCE FAILURE
Jnoicates that the selected navigation
source has faded. An navigation
source related displays are removed.
Displayed in red.
See L A U I.
EKS1
LOC FAILURE ANNUNCIATOR
Replaces t he locaiizer/rising runway
pointer and scale when the localizer
signal is not valid. Displayed in red.
y—K-bcj i
EADI
PILOTS AND COPILOTS INSTRUMENT PANELS
GS FAILURE ANNUNCIATOR
Replaces the gfcdestope scale and
pointer when the ghdeslope signal is
not valid. Displayed in red.
VHF/NAV System - EFIS Failure Displays
Figure 26
SECTION 16
Page 32
Apr 02/87
canaaair
ciiaueneter
OPERATING MANUAL
PSP 601A-6
PILOTS AND COPILOT'S
MICROPHONE AND
HEADPHONE JACKS
O
MAV 1 MONITOR
SWITCH
Selects (up position)
VHF/NAV 1 audio for
presentation on the
speaker and/or
headphones.
& 1 ^SPKR/PHONE SWITCH
Switches audio to speaker.
headphones, or both.
NAV 2 MONITOR SWITCH
Selects (up position) VHF/NAV 2
audio for presentation on the
speaker and/or headphones.
MKR 1 MONITOR SWITCH
Selects (up position) marker beacon
audio from the VHF/NAV 1 for
presentation on the speaker and/or
headphones.
MKR 2 MONITOR SWITCH
Selects (up position} marker beacon
audio from VHF/NAV 2 for
presentation on the speaker and/or
headphones.
HF
1 2
VHF
1 2 p^O QQQQQQQQ QQ
2 HFl HF
HOTOXY 1Y'P=Ix\ INPH O a MIC BOOM
MIC
NOTE
/ » \ K power fails on either channel of the audio
eJectfuwcs unit, the controls wiH not
function.
Emergency Operation: Pilot can use VHF 1
and hear NAV 1 without volume control.
Copilot can use VHF 2 and hear NAV 2
without volume control.
A SPKR VOL CONTROL
Varies volume of audio to speaker
and headphones except aural
warning. Turn clockwise to increase
volume.
PILOTS AND COPILOT'S SIDE CONSOLE
VHF/NAV System Audio Selection/Control
Audio Integrating System
Figure 27
SECTION 16
Page 33
Apr 02/87
OPERATING MANUAL
PSP 601A-6
I ADM
AOF2
1 AUDIO
INTEGRATING
SYSTEM
PILOT'S ERS
1 •" "i
AUDIO
INTEGRATING
SYSTEM
—#~
>
>
DISPLAY
CONTROLLER
ADF1
* ^
t
BRG o
o
! a' ° * ©
! ADF2J 6
i BRG 0
COPILOTS EFIS
DISPLAY
CONTROLLER
ADF1
% o
6
BRG o
• " • • —^o \
ADF2
BRGO
t ^
I
A
„
\
PILOTS B1SI
COPILOTS EHSI
ADF System - Simplified Block Diagram
Figure 28
SECTION 16
Page 34
Apr 02/87
ctiauencjer
OPERATING MANUAL
PSP 601A-6
COMPARATOR ANNUNCIATOR
Rashes when receiver tunes TO an
ADF frequency not the same as the
active frequency displayed.
PRESET FREQUENCY DISPLAY
Indicates preset frequencies and
diagnostic messages.
MEMORY ANNUNCIATOR
Indicates a preset frequency ts
displayed on the preset frequency
display.
VOLUME CONTROL
Adjust audio level.
ACTIVE FREQUENCY DISPLAY
indicates active frequencies and
diagnostic messages.
POWER AND MODE SWITCH
Turns on ADF receiver and selects
operating mode.
LIGHT SENSOR
XFR/MEM SWITCH
Transfers active and r"—
frequencies or seiects pteset
frequency for display.
Adjusts brightness of controls and
displays.
TEST PUSHBUTTON
initiates self-test routine.
FREQUENCY SELECTORS
Selects preset and active
frequencies.
ACT PUSHBUTTON
Allow frequency selectors to directly
tune ADF receiver.
STO PUSHBUTTON
Allows frequencies to be selected
and stored in memory.
CENTRE PEDESTAL
ADF System Control Unit SECTION 16
Figure 29 Page 35
Apr 02/87
OPERATING MANUAL
PSP 601A-6
BRGO AND BRG O SELECTORS
When set to AOF 1. the associated bearing pointer
on the BtSI displays the bearing to the station
tuned on the AOF system No. 1. When set to AOF
Z the associated bearing pointer on the EHSl
displays the bearing to the station tuned on the
ADF system No. 2.
PILOTS AND COPILOTS SIDE PANELS
ADF System SouTce Selection -
EFIS Display Control!er
Figure 30
SECTION 16
Page 36
Apr 02/87
cacntiaaanaetnr Qer
OPERATING MANUAL
PSP 601A-6
BEARING POINTERS
Display bearing selected
on the display controller.
BEARING SOURCE
ANNUNCIATORS
Indicate the sources used
for the bearing pointers.
N1
FMS
180
SALON
\ TTG
34.5
• / ^ i
^ \_[ J
PILOTS AND COPILOT'S INSTRUMENT PANELS
ADF System EFIS Displays
Figure 31
SECTION 16
Page 37
Apr 02/87
OPERATING MANUAL
PSP 601A-6
PILOTS AND COPILOTS
MICROPHONE AND
HEADPHONE JACKS
O
A \ SPKR/PHONE SWITCH
Switches auobo to speaker,
headphones, or both.
AOF 1 MONITOR SWITCH
Selects (up position) AOF 1 audio
for presentation on the speaker
and/or headphones.
ADF 2 MONITOR SWITCH
Selects (up position) AOF 2 audio
for presentation on the speaker
L and/or headphones.
I NAV MKR fADFl HF VHF |
PQQOQQQQQOQQ
OFF
SPKR DME
SPKR/?=^\ 1 2 HOT OXY V
MIC BOOM
2 HF1 HF
-INPH
MJC a
A
A N O T I
/ l \ tf power fafe on either channel of the audio
eJectioracs unit, the controls w£B not
function.
Emergency Operation: Piot can use VHF 1
and hear NAV 1 without volume control.
Copilot can use VHF 2 and hear NAV 2
without volume control.
SPKR VOL CONTOL
Varies volume of audio to speaker
and headphones except aural
warning. Turn clockwise to increase
PILOTS AND COPILOTS SIDE CONSOLE
ADF System Audio Selection/Control -
Audio Integrating System
Figure 32
SECTION 16
Page 38
Apr 02/87
canattair
OPERATING MANUAL
PSP 601A-6
• TO AUDIO INTEGRATING
SYSTEM
COPILOT'S
DISPLAY
CONTROLLER
^* TO AUDIO INTEGRATING
SYSTEM
PILOT'S EHSI
MFD
I X
COPILOTS EHSI
DME System - Simplified Block Diagram
Figure 33
SECTION 16
Page 39
Apr 02/87
OPERATING MANUAL
PSP 601A-6
PRESET FREQUENCY DISPLAY
Displays preset (inactive) frequency
and diagnostic messages. Shews
DME frequency when HID is
ACT ANNUNCIATOR
Conies on while the active frequency
is changed. Stays on flashing if the
tuning is Kicorrect.
MEMORY ANNUNCIATOR
Comes on when a preset frequency
is shown in the preset frequency
display.
RMT ANNUNCIATOR
Comes on while the DME is remotely
tuned by the FMS.
POWER AND MODE SELECTOR
OFF - Removes power from the
DME and VOR systems.
ON - Applies power to the DME and
VOR systems.
HLD - Holds the DME on the
selected frequency white the
VHF/NAV frequency is changed.
ACTIVE FREQUENCY DISPLAY
Displays active frequency and
diagnostic messages.
XFR/MEM SWITCH
AHows transfer of a preset frequency
into the active display (XFR
position). Loads stacked memory
frequency into preset display (MEM
position).
HLD ANNUNCIATOR
Comes on to indicate that the DME
is held while VHF/NAV frequency is
changed.
FREQUENCY SELECTORS
Selects the DME and VOR
frequencies simultaneously.
ACT PUSHBUTTON
Enables the frequency selectors to
directly tune the DME and
VHF/NAV.
LIGHT SENSOR
Automatic display dimming sensor
STORE PUSHBUTTON
Allows preset frequencies to be
selected and entered into memory.
TEST PUSHBUTTON
Initiates the serf-test diagnostic
routine on the DME system.
CENTRE PEDESTAL
DME System Selection/Control - VHF/NAV Control
Figure 34
SECTION 16
Page 40
Apr 02/87
chanencjer
OPERATING MANUAL
PSP 601A-6
/ tf CRS 35
DME HOLD
ANNUNCIATOR
Indicates that the DME
hold function is selected.
^ X
DMEH
180
SALON J
o
/
DME IDENTIFIER
Displays the DME station identifier
for the distance displayed. Displayed
in green or yeilow consistent with
the distance display.
DISTANCE DISPLAY
Displays the DME distance to the
selected VHF/NAV source. When
the on-side VHF/NAV source is
selected, the distance display is
green. When the cross-side
VHF/NAV source is selected, the
display is yellow.
PILOT'S AND COPILOTS INSTRUMENT PANELS
DME System - EFIS Displays
Figure 35
SECTION 16
Page 41
Apr 02/87
OPERATING MANUAL
PSP 601A-6
PILOTS AND COPILOTS
MICROPHONE AND
HEADPHONE JACKS
©
A SPKR/PHONE SWITCH
Switches audio to speaker,
headphones, or both.
C=CFI
NAV MKR ADF HF VHP
P Q0Q 9 9Q8 Q Q 0 0
SPKR DME OFF
SPKR/?=^\ 1 2 HOT OXY
MIC BOOM MIC
A SPKR VOL CONTOL
Varies volume of audio to speaker
and headphones except aural
warning. Turn clockwise to increase
volume.
OME 2 MONITOR SWITCH
Selects (up position) DME 2 audio
for presentation on the speaker
and/or headphones.
AS
NOTE
power fate on either channel of the audio
etectrorecs unit, the controls wffi not
function.
Emergency Operation: Wot can use VHP 1
and hear NAV 1 without volume control.
Copilot can use VHP 2 and hear NAV 2
without volume control.
OME 1 MONITOR SWITCH
Selects (up position) DME 1 audio
for presentation on the speaker
and/or headphones.
PILOTS AND COPILOTS SIDE CONSOLE
DME System Audio Selection/Control -
Audio Integrating System
Figure 36
SECTION 16
Page 42
Apr 02787
e^iaiiehcrer
OPERATING MANUAL
PSP 601A-6
ALTITUDE DISPLAY
Displays the encoder altitude or the
two-digit fault code.
CODE DISPLAY
Displays the selected code or
diagnostic readout in case of failure.
ACT ANNUNCIATOR
Comes on while the codes are
changed and Dashes when the reply
code does not match the displayed
code.
TX ANNNOATOR
Comes on each time the transponder
replies to an interrogation
MODE SELECTOR
OFF position: Removes power from
the transponder.
STBY position: Enables reception
and disables transmission.
ON position: Enables reception and
transmission.
ALT position: Enables reception
and transmission and transmits
barometric attitude in response to a
mode C request.
1/2 TRANSPONDER SELECTOR
In position 1. enables the ATC 1
transponder. In position 2, enables
the ATC 2 transponder.
OUTER CODE SELECTOR
Selects the first and second digits of
the reply code.
INNER CODE SELECTOR
Selects the third and fourth digits of
the reply code.
PRE PUSHBUTTON
Enables the selected preset code to
be stored in the non-votatile memory
and recalls stored code for display.
DIMMING SENSOR
Automatically controls the brightness
of the displays.
1DENT PUSHBUTTON
Initiates transmission of a special
idem pulse to the ground radar.
TEST PUSHBUTTON
Initiates the transponder self-test
routine.
CENTRE PEDESTAL
ATC Transponder System Control Unit SECTION 16
Figure 37 Page 43
Apr 02/87
OPERATING MANUAL
PSP 601A-6
K.U>. ii - r.c>
COPILOTS &ISI
FMS - Simplified Block Diagram
Figure 38
SECTION 16
Page 44
Apr 02/87
OPERATING MANUAL
PSP 601A-6
OR ANNUNCIATOR
Indicates that the DME
updating and IRS position
information are tost and
the FMS is operating in
the dead reckoning mode.
DSPLY ANNUNCIATOR
Indicates that the
information on the CDU is
for display only, and is not
being used for navigation.
PERF MODE KEY
Calls up page 1 of the
performance index (PERF
INDEX) pages for display
on the CDU.
NAV MODE KEY
Calls up page 1 of the
navigation index (NAV
INDEX) pages.
PREV AND NEXT KEYS
Use to select the previous
(PREV) or next (NEXT)
screen (page) for display
on the CDU.
DEGRAD ANNUNCIATOR
Indicates that the FMS is
operating in a degraded
mode. Accuracy of the
display data cannot be
guaranteed.
C Q j ^ M r ^ "11 oouon 1 «sc 11 o*snl ? «*»"] Q
MSG ANNUNCIATOR
Indicates that an active
message is displayed in the
scratchpad.
OFFSET ANNUNCIATOR
Indicates that an offset
from the desired track has
been entered on the
PROGRESS page.
ACTIVE FLT PLAN i/s
D£S7
ML F KSLC
020' 93 0 N V AiO i
SLC 0r*!tV '<*J JV?;J
A^ClVAL is
q
C3E3EJ
00
^Q
S®
SB
APRCH ANNUNCIATOR
Indicates that the FMS is
operating in the approach
(high sensitivity) mode.
DIR MODE KEY
Calls up page 1 of the
active flight plan with
direct to (DIRECT) and
INTERCEPT prompts.
PROG MODE KEY
Calls up page 1 of the
progress (PROGRESS)
pages for display on the
CDU.
FPL MODE KEY
Calls up page 1 of the
active flight plan (ACTIVE
FLT PLAN) pages.
CENTRE PEDESTAL
FMS Control Display Unit (CDU) SECTION 16
Figure 39 (Sheet 1) Page 45
Apr 02/87
OPERATING MANUAL
PSP601A-6
UNE SELECT KEYS
Call up the CPU display
for tho wdoxod item.
SCRATCHPAD
Provides display area for
the entry of data and/or
the venficaDon of data
before ine selection.
ALPHANUMERIC KEYS
Provide for the entry of
numeric and alphabetic
data.
PHOTO SBISORS
/UxtomaocaOy maimain the display
intensity with respect to
lighting.
ACTIVE FIT PLAN 1/5
OEST
MLF KSLC <j
020° 93 0NM 610 4.
SLC 09102 160/4920 t
348° 4.0 MM
KSLC 09U2 4560
<]A«MAITN! ARRIVAL >
0 0 0 0 0 0 © ® ®
© 0 0 3 0 0 0 0 0 0
© 0 0 0 0 0 0 0®
h 0 S 0 0 ® 0 ® .^ Psssee ©0
DEL KEY
CLRKEY
1 m conjunction with
the ine select keys in
order to delete fine items
from the CDU.
UNE SELECT KEYS
CaU up the CDU dlsptay
for the indexed item.
BRT CONTROL
Adjusts the CDU display
intensity.
the
FMS Control Display Unit (CDU) SECTION 16
Figure 39 (Sheet 2) Page 46
Apr 02/87
OPERATING MANUAL
PSP 601A-6
GSPD/TTG PUSHBUTTON
Selects between ground speed
(6SPD) and time-to-go (TTG) for
display on the EHSl. Ground speed
is supplied by the FMS when the
FMS navigation source is selected. FMS PUSHBUTTON
Selects between FMS 1 or FMS 2
navigation source for display on the
EHSL
BRGO SELECTOR
When set to FMS "5 the bearing
pointer displays bearing from the
No. 1 FMS. BRGO SELECTOR
When set to FMS 2 the bearing
pointer displays bearing from the
No. 2 FMS.
PILOT'S AND COPILOT'S SIDE PANELS
FMS EHSI Source Selection -
EFIS Display Controller
Figure 40
SECTION 16
Page 47
Apr 02/87
OPERATING MANUAL
PSP 601A-6
LAT WPT ANNUNCIATOR
Comes on to indicate that the
diiaafi is within 30 seconds of the
next lateral waypoint and goes out
when the aircraft reaches the
waypoint.
nsH
. RESET _
] l 1
|]i i
li i i
i i i
VERT WPT ANNUNCIATOR
Comes on to indicate that the
aircraft is within 1000 feet of the
vertical waypoint (VNAV) and goes
out when the aircraft reaches the
waypoint.
n
JuTiiFr]
! VBTT I
OFFSET^
OFFSET ANNUNCIATOR
Comes on when a lateral offset path
is entered on the PROGRESS page
of the CDU and goes out when the
offset function is removed.
r— HttSSTOSEttCT -,
FMS TUNE MAN/FMS
SWITCH/LIGHT
Selects the manual or auto-tune
function.
PILOTS AND COPILOTS INSTRUMENT PANELS
FMS - Remote Annunciators
Figure 41
SECTION 16
Page 48
Apr 02/87
OPERATING MANUAL
PSP 601A-6
VTA ANNUNCIATOR
Indicates (Hashing) a FMS vertical
waypoint passage. Comes on 30
seconds prior to waypoint passage.
Displayed in magenta.
FMS SPEED BUG
Indicates the FMS reference speed.
Displayed in magenta.
VERTICAL NAVIGATION POINTER
AND SCALE
Indicates the aircrafts deviation from
the FMS computed vertical path.
Displayed in magenta.
PILOTS AND COPILOT'S INSTRUMENT PANELS
NOTE
When the vertical navigation function fails, the vertical
navigation pointer and scale is removed.
FMS - EADI Display
Figure 42
SECTION 16
Page 49
Apr 02/87
OPERATING MANUAL
PSP 601A-6
NAVIGATION SOURCE
ANNUNCIATOR
Indicates the selected navigation
source. When the on-side FMS
source is selected, the annunciator is
green, when the cross-side FMS
source is selected, the annunciator is
yellow (see note).
BEARING POINT NO. 1
Indicates the bearing to the source
selected by the BRG Q control.
Displayed in cyan.
BEARING POINTER NO. 2
Indicates the bearing to the source
selected by the BRG O selector.
Displayed in white.
BEARING SOURCE
ANNUNCIATORS
tadJcates the selected bearing source
for the associated bearing pointer.
A = ADF
f = FMS
V = VOR
V ne color of the bearing source
annunciators correspond to the
bearing pointers.
DESIRED TRACK BAR AND
POINTER
Indicates aircraft deviation from the
FMS desired track. The pointer is
displayed in green or yellow
(consistent with the navigation
source annunciator}.
P I L O T S AND COPILOTS INSTRUMENT PANELS
NOTE
When the FMS navigation
and the navigation source
fails all related displays are removed
is displayed in red in a red box.
FMS - EHSI Full Compass Display
Figure 43 (Sheet 1)
SECTION 16
Page 50
Apr 02/87
ctiauenper
OPERATING MANUAL
PSP 601A-6
MSG ANNUNCIATOR
Indicates thai an active message is
displayed on the FMS COU.
DTK DISPLAY
Provides a numeric readout of the
desired track pointer position with
respect to the heading dial.
Displayed in green or yellow
(consistent with the navigation
source annunciator}.
TO/FROM ANNUNCIATOR
indicates whether the aircraft is
moving towards or away from the
FMS waypoint. Displayed in green
or yellow (consistent with the
navigation source annunciator).
DISTANCE DISPLAY
Displays the FMS distance to the TO
waypoint. Displayed in green or
yellow (consistent with the
navigation source annunciator}.
angle computed
GSPD DISPLAY
Displays ground speed calculated by
the FMS (see note}.
WAYPOINT IDENTIFIER
Displays the waypoint identifier for
the distance displayed. Displayed in
green or yellow (consistent with the
navigation source annunciator).
NOTE
Ground speed is supplied by the IRS when the FMS navigation source is not selected.
FMS - EHSI Full Compass Display
Figure 43 (Sheet 2)
SECTION 16
Page 51
Apr 02/87
OPERATING MANUAL
PSP 601A-6
/ , r DTK
010 1 0 5 ^ ? MAG pf] HDG
r^r1 020
WAYPOINTS AND
TRACK UNES
Indicate the FMS flight
plan. Displayed in green.
CROSS-TRACK
DISTANCE DISPLAY
Indicates the aircrafts
deviation from the desired
track in nautical mi&es.
Displayed in green or
yettow (consistent with the
TO/FR annunciators).
WAYPOINT FLIGHT
LEVEL CONSTRAINT
If applicable, indicates the
flight levei constraint for
the TO waypoint.
TO WAYPOINT AND
IDENTIFIER
The TO waypoint is
displayed in magenta and
the identifier for the TO
waypoint is displayed in
green.
TO/FR ANNUNCIATORS
Indicates whether the
aircraft is moving towards
(TO) or away from (FR)
the FMS waypoint.
Displayed in green when
the FMS navigation source
is on-side and in yellow
when the FMS navigation
source is cross-side.
PILOTS AND COPILOTS INSTRUMENT PANELS
NOTE
T*ie map mode provides the same information as the full compass
mode, except that the course pointer, scale and deviation bar are
removed and a partial compass is displayed with the additional
information indicated in this figure.
FMS - EHSI MAP Display (Additional Displays)
Figure 44
SECTION 16
Page 52
Apr 02/87
OPERATING MANUAL
PSP 601A-6
SRC PUSHBUTTON
Selects between the FMS 1 and
FMS 2 navigation source for display
on the MFD.
MAP/PLAN PUSHBUTTON
Selects between the MAP and PLAN
displays for the MFD.
Positions the designator on the
MFD.
RCL PUSHBUTTON
INC/DEC RNG
Selects the displayed range. When
weather radar returns are displayed
the range is controlled by the
weather radar controller.
APT PUSHBUTTON
Recalls the designator to it's home
position.
SKP PUSHBUTTON
When pressed, causes the
designator to make the next
waypoim it's home position.
Controls the bnghtness of the MFD
display.
ENT PUSHBUTTON
Enters the designator position into
the FMS flight plan as the TO
waypoim.
Selects airports for display on the
MFD.
DAT PUSHBUTTON
Adds long range navigation
information to the MFD.
CENTRE PEDESTAL
FMS MFD Source Selection and Display Control -
EFIS MFD Controller
Figure 45
SECTION 16
Page 53
Apr 02/87
OPERATING MANUAL
PSP 601A-6
HEADING SOURCE ANNUNCIATOR
A white MAG annunciation is
displayed above the heaomg dial to
indicate that the heading source is
referenced to magnetic North.
DISTANCE AND COURSE TO
DESIGNATOR DISPLAY
Displays the course and distance to
the designator, when the designator
is offset. Displayed in cyan.
WAYPOINTS AND TRACK LINES
indicate the FMS flight plan. The TO
waypomi is displayed in magenta
and an other waypoints are displayed
in white. The active track line is
displayed in green and all other track
lines ate displayed in white.
AIRPORT SYMBOL
Identifies the locations of airports.|
Displayed in white.
VOR/DME NAVAID
Identifies the locations of VOR/DME
stations. Displayed in white.
DESIGNATOR LATITUDE/
LONGITUDE DISPLAY
NAVIGATION SOURCE
ANNUNCIATOR
indicates the FMS navigation source
selected on the MFD controller.
Displayed in green.
TO WAYPOINT IDENTIFIER
Identifies the TO waypoint.
Displayed in green.
ETA/TTG DISPLAY
Displays estimated time-of -arrival
(ETA) or ©me-to-go (TTG) for the
TO waypoint. Displayed in green.
Indicates the aircraft deviation from
the desired track in nautical miles.
Displayed in green.
Displays the coordinates of the
designator, frsptayed in green.
DESIGNATOR AND
DISPLACEMENT LINE
Used in conjunction with the MFD
controller joystick in order to alter
the flight plan. Displayed in white in
it's home position and in cyan when
offset.
DISTANCE DISPLAY
Indicates the distance to the TO
waypoint. Displayed in green.
CENTRE INSTRUMENT PANEL
FMS - MFD MAP Display
Figure 46
SECTION 16
Page 54
Apr 02/87
cttauenaer
OPERATING MANUAL
PSP 601A-6
DISTANCE AND COURSE TO
DESIGNATOR DISPLAY
Displays the course and distance to
the designator, when the designator
is offset. Displayed in cyan.
HEADING SOURCE ANNUNCIATOR
A white MAG annunciation is
Displayed to indicate that the
heading source is referenced to true
magnetic North.
WAYP01NTS AND TRACK LINES
Indicate the FMS flight plan. The TO
waypomt is displayed in magenta
and all other waypomts are displayed
in white. The active track line is
displayed in green and all other track
lines are displayed in white.
NORTH UP ANNUNCIATOR
Indicates that the North-up
(PLAN) mode is selected.
DESIGNATOR LATITUDE/
LONGITUDE DISPLAY
Displays the coordinates of the
designator. Displayed in green.
NAVIGATION SOURCE ANNUNCIATOR
indicates the FMS navigation source
selected on the MFD controller.
Displayed in green.
RANGE RING AND RNG
ANNUNCIATOR
Indicates the selected range
DESIGNATOR AND
DISPLACEMENT LINE
Used in conjunction with the MFD
controller joystick in order to after
the flight plan. Displayed in white in
it's home position and in cyan when
offset.
TO WAYPOINT IDENTIFIER
Identifies the TO waypotnt.
Displayed in green.
ETA/TTG DISPLAY
Displays estimated time-of-arrivai
(ETA) or time-to-go (TTG) for the
TO waypomt. Displayed tn green.
DISTANCE DISPLAY
Indicates the distance to the TO
waypotnt. Displayed in green.
CENTRE INSTRUMENT PANEL
FMS - MFD PUN Display
Figure 47
SECTION 16
Page 55
Apr 02/87
OPERATING MANUAL
PSP 601A-6
SET SWITCH
UP - advances dock one second for
each second held.
D - retards dock one second for
each second held.
BRIGHT/DIM SWITCH
S - brightens display.
DIM - dims display.
1 HR UP - advances time one-hour
when held and released.
PRESS TO
RESET
PRESS TO RESET PUSHBUTTON
Allows flight time recorder to be
reset to zero without turning off
aircraft electrical power.
TIME SWITCH
TIME - displays selected standard
time.
F.T. - displays flight tvne.
£-T. - displays elapsed time.
HOURS AND MINUTES
DISPLAY
ELAPSED TIME SWITCH
RUN - starts elapsed time meter.
STOP - stops elapsed time meter.
ZERO - returns elapsed time meter
to zero when held and released. Also
returns flight time meter to zero
when the aircraft is on the ground.
PILOTS AND COPILOTS SIDE PANELS
Digital Clock Controls SECTION 16
Figure 48 Page 56
Apr 02/87 |
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